IRIDIUM 106, 41917
Orbit data source: Space-Track
IRIDIUM 106, 41917 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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41917 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 IRIDIUM 106
1 41917U 17003A 25300.41747855 .00000168 00000-0 52948-4 0 9991
2 41917 86.4031 185.7869 0001700 73.9344 286.2039 14.34218505459841Epoch: 2025-10-27T10:01Z
TLE epoch observation values (Epoch: 2025-10-27T10:01:10.146Z)
Latitude
-0.00003°
Longitude
-0.525°
Altitude
780.376 km
Speed
7.464 km/s
True Right ascension
12h 23m 08s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:18:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.845 km
Perigee altitude
773.413 km
Semi-major axis
7,152.766 km
Eccentricity
0.00017
Inclination
86.4031°
RAAN
185.7869°
Arg. of periapsis
73.9344°
True anomaly
286.18519°
Mean anomaly
286.2039°
Eccentric anomaly
286.19455°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000052948
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 106 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-28 16:16:58.966Z | 143.022° SSE | 2025-10-28 16:20:58.966Z | 79.523° E | 29.066° | 2025-10-28 16:24:58.966Z | 23.659° NE |
| 6 mins | 2025-10-28 17:58:58.966Z | 240.772° WSW | 2025-10-28 18:01:58.966Z | 290.004° WNW | 23.166° | 2025-10-28 18:04:58.966Z | 330.823° NNW |
| 9 mins | 2025-10-29 04:27:58.966Z | 1.238° NNE | 2025-10-29 04:31:58.966Z | 111.507° ESE | 44.477° | 2025-10-29 04:36:58.966Z | 174.891° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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